EP0642855B1 - Casting mold - Google Patents

Casting mold Download PDF

Info

Publication number
EP0642855B1
EP0642855B1 EP94113405A EP94113405A EP0642855B1 EP 0642855 B1 EP0642855 B1 EP 0642855B1 EP 94113405 A EP94113405 A EP 94113405A EP 94113405 A EP94113405 A EP 94113405A EP 0642855 B1 EP0642855 B1 EP 0642855B1
Authority
EP
European Patent Office
Prior art keywords
core
molten metal
cast
casting
weight
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
EP94113405A
Other languages
German (de)
French (fr)
Other versions
EP0642855A1 (en
Inventor
Atsushi Ota
Seizi Uda
Shingo Nakamura
Hidehiko Kadono
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Toyota Motor Corp
Original Assignee
Toyota Motor Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Toyota Motor Corp filed Critical Toyota Motor Corp
Publication of EP0642855A1 publication Critical patent/EP0642855A1/en
Application granted granted Critical
Publication of EP0642855B1 publication Critical patent/EP0642855B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22CFOUNDRY MOULDING
    • B22C9/00Moulds or cores; Moulding processes
    • B22C9/10Cores; Manufacture or installation of cores
    • B22C9/101Permanent cores
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D15/00Casting using a mould or core of which a part significant to the process is of high thermal conductivity, e.g. chill casting; Moulds or accessories specially adapted therefor
    • B22D15/02Casting using a mould or core of which a part significant to the process is of high thermal conductivity, e.g. chill casting; Moulds or accessories specially adapted therefor of cylinders, pistons, bearing shells or like thin-walled objects
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D17/00Pressure die casting or injection die casting, i.e. casting in which the metal is forced into a mould under high pressure
    • B22D17/20Accessories: Details
    • B22D17/22Dies; Die plates; Die supports; Cooling equipment for dies; Accessories for loosening and ejecting castings from dies
    • B22D17/24Accessories for locating and holding cores or inserts
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D19/00Casting in, on, or around objects which form part of the product
    • B22D19/0009Cylinders, pistons

Definitions

  • the present invention relates to a method used to produce a cast product having a concave portion, e.g., a hole or the like, therein.
  • a core or a core pin has been used conventionally when producing a cast product which has a concave portion such as a hole or the like therein.
  • the core or the core pin is subjected to a holding force which results from the shrinkage of a molten metal during solidification. Accordingly, it is difficult to remove the core or the core pin from the resulting cast product after cooling the cast product.
  • it is usually tapered gradually from wide to narrow in the direction toward its leading end.
  • the cast products When the cast products are produced by using the core or the core pin, they come to have a concave portion such as a hole or the like.
  • the resulting concave portion is inevitably formed in a tapered hole whose inside diameter reduces from large to small in the direction toward its inner side.
  • it is hard to make the resulting concave portion which has an identical inside diameter over its entire length.
  • it is a routine practice to carry out machining on the inner periphery of the concave portion after the casting, thereby establishing an identical inside diameter over the entire length of the concave portion.
  • the molten aluminum or zinc is solidified rapidly at its surface where it is brought into contact with a mold. Consequently, at the surface where the molten aluminum or zinc is brought into contact with the mold, there is formed a healthy layer in which no bubbles are involved in a thickness of from about 0.7 to 1.0 mm.
  • blow holes in the deeper layer disposed under the healthy layer because the molten aluminum or zinc is solidified at a slower rate in the deeper layer.
  • the machining allowance should be enlarged on the inner side of the concave portion so that it goes beyond the healthy layer.
  • the blow holes come to be exposed to produce defects.
  • the concave portion should be machined in excess of about 3.49 mm at its innermost portion. Accordingly, the concave portion is machined completely beyond the healthy layer.
  • a casting process using a cast insert member has been known, in which casting is carried out after a cast insert member e.g., a liner or the like, formed independently is disposed in a cavity.
  • a cast insert member e.g., a liner or the like
  • casting is carried out after disposing a protective member in a cast insert member. If such is the case, there should be provided a clearance between the cast insert member and the protective member. Consequently, it is difficult to completely get rid of the deformation in the cast insert member.
  • the protective member in order to prevent the protective member from being stuck in the cast insert member due to the deformation in the cast insert member, the protective member should be formed in a configuration having a draft taper. Consequently, when the cast insert member is deformed to conform to the configuration of the protective member, it is required to machine the inner periphery of the cast insert member after casting, and at the same time, there occur problems in that the machining has resulted in the partially fluctuating thickness in the cast insert member. Furthermore, there are produced defects which result from the molten metal invasion into the clearance between the cast insert member and the protective member.
  • DE-C-973984 discloses a casting core made of light metal and having a coefficient of expansion which is larger than the amount of shrinkage of a molten material. While cooling, the solidifying alloy shrinks less than the core. Thus, the core can easily be detached from the cast product.
  • the core is of light metal, it can be provided with an oxide film on its outer periphery or cooled by means of a liquid which is leaded through a bore within the core.
  • the oxide film or the liquid cooling are only used to prohibit the core from melting. Therefore, the cooling of the core is used to hold the temperature of the core some less the melting point of the core-material. Thus, the temperature of the core while solidifying of the cast product is nearly the same as the temperature of the cast product.
  • JP -A- 63144845 a similar casting method is known.
  • This method also uses a core having a thermal expansion coefficient which is greater than that of the casting material.
  • the core is preheated to a prescribed temperature which is adapted -on the one hand- to the average temperatures of the components when solidification starts, and -on the other hand- to the difference in the thermal expansion coefficients.
  • the present invention is developed in view of the aforementioned circumstances. It is therefore an object of the present invention to provide a method for producing a cast product with a concave portion which still allows to give the concave portion an inside diameter as identical as possible over its entire length and to reduce a machining allowance after casting, and which leads reliably to a large enough clearance between the core and the cast product, even with a broad range of cast materials.
  • the core further includes a casting insert member disposed around its outer periphery.
  • the core greatly expands thermally during casting. While it keeps the expanded state, the molten metal starts solidifying. Accordingly, the molten metal is subjected to a pressing force resulting from the expansion of the core during its solidification process. With the present casting mold, it is possible to inhibit the defects like the shrinkage cavities and so on from producing in the resulting cast products.
  • the core shrinks more than the molten metal adjacent thereto does. Consequently, there arises a clearance between the outer peripheral surface of the core and the inner peripheral surface of the concave portion formed by the core in the resulting casting products. As a result, even when the untapered configuration is given to the core, it is possible to remove the core from the concave portion with ease and to reduce the machining allowance in the concave portion which has been usually required after casting.
  • the core includes the cast insert member disposed on its outer periphery as done in the preferred form of the present casting mold
  • casting is carried out while the core is fitted into the cast insert member.
  • the core expands greatly, thereby outwardly pressing the inner peripheral surface of the cast insert member.
  • it is possible to reduce the clearance between the cast insert member and the core to zero.
  • it is possible to inhibit the cast insert member from being deformed by the shrinkage stress of the molten metal and to prohibit the molten metal from invading between the cast insert member and the core.
  • the core shrinks considerably to thereby produce a clearance between itself and the cast insert member. Consequently, it is possible to remove the core from the cast insert member with ease. Therefore, it is unnecessary to give the conventional tapered configuration to the core. Thus, it is possible to get rid of the step of machining the cast insert member after casting.
  • the cast insert member is inhibited from being deformed by the shrinkage force of the molten metal. Accordingly, it is possible to get rid of the step of machining the cast insert member after the casting and to prevent the strength of the cast insert member from being deteriorated.
  • FIG. 1 there is illustrated a schematic cross-sectional view of a casting mold of a First Preferred Embodiment according to the present invention.
  • the casting mold comprises a pair of main molds 1, 2, a cavity 10 formed by the main molds 1, 2, and a cylindrical slider pin 3 disposed in the cavity 10.
  • the casting mold is used for casting an aluminum die-cast component part.
  • the slider pin 3 is formed of a high-manganese-content alloy which includes Mn in an amount of 22% by weight.
  • Casting was carried out by charging a molten aluminum alloy into the casting mold constructed as described above.
  • Figure 2 there are illustrated a variation of the temperature of the molten aluminum alloy (or a cast product) with the time elapsed and a variation of the temperature of the slider pin 3 therewith.
  • the temperature of the molten aluminum alloy decreased gradually, but the temperature of the slider pin 3 increased sharply so as to approach the temperature of the molten aluminum alloy. Since the slider pin 3 exhibited a thermal expansion coefficient greater than that of the molten aluminum alloy, the slider pin 3 expanded to apply a pressing force to the molten aluminum alloy.
  • FIG 4 there is illustrated a casting mold which has been used conventionally.
  • a slider pin 3' was employed which had a maximum diameter of 30 mm. Since it was formed of a steel, it exhibited a thermal expansion coefficient smaller than that of the molten aluminum alloy.
  • the slider pin 3' was provided with a draft angle of 1 degree in order to make it likely to be removed from the cast product.
  • the slider pin 3 could be removed from the cast product with ease even when it had a maximum diameter of 30 mm and it was provided with a draft angle of 15 minutes. If such was the case, it was necessary to machine the inner periphery of the hole portion only by a machining allowance of 0.8 mm at maximum after the casting. Therefore, it was possible to inhibit the material from being wasted, and at the same time there was produced no defect resulting from the shrinkage cavities.
  • the slider pin 3 for casting an aluminum die-cast component part can be made from either a high-manganese-content alloy which includes Mn in an amount of from 10 to 25% by weight, C in an amount of from 0.2 to 1.5% by weight, Cr in an amount of from 1 to 3% by weight, and the balance of Fe and inevitable impurities, an austenite stainless steel, or a bimetallic alloy which includes Mn in an amount of from 65 to 80% by weight, Cr in an amount of from 10 to 20% by weight, and the balance of Ni and inevitable impurities.
  • a high-manganese-content alloy which includes Mn in an amount of from 10 to 25% by weight, C in an amount of from 0.2 to 1.5% by weight, Cr in an amount of from 1 to 3% by weight, and the balance of Fe and inevitable impurities
  • an austenite stainless steel or a bimetallic alloy which includes Mn in an amount of from 65 to 80% by weight, Cr in an amount of from 10 to 20% by weight, and the balance of Ni and inevitable impur
  • FIG 3 there is illustrated a schematic cross-sectional view of a casting mold of a Second Preferred Embodiment according to the present invention.
  • the casting mold is designed to cast an automotive engine block, one of the aluminum die-cast component parts. It comprises an upper mold 40, a lower mold 41, and a pair of slider cores 42, 42. Between the upper mold 40 and the lower mold 41, there is disposed a liner 5 (i.e., the cast insert member) for constituting an inner peripheral surface of a bore. Moreover, a core 6 is held by the upper mold 40 at one of the opposite ends, and it is fitted into the liner 5.
  • a liner 5 i.e., the cast insert member
  • the liner 5 is made from a steel.
  • the core 6 is formed of a bimetallic alloy which includes Mn in an amount of 68% by weight, and accordingly it exhibits a thermal expansion coefficient remarkably larger than those of the liner 5 and the resulting cast product. Moreover, when cooled, the core 6 is designed so that it has an outside diameter slightly smaller than the inside diameter of the liner 5.
  • the liner 5 and the core 6 were expanded by the heat of the molten aluminum alloy. Since the core 6 exhibited a thermal expansion coefficient remarkably larger than that of the liner 5, it contacted with the inner periphery of the liner 5 to press the liner 5 in the expanding direction. Thus, the clearance disappeared, and accordingly the molten aluminum alloy barely invaded between the liner 5 and the core 6. Moreover, the expanding stress arisen in the liner 5 was conveyed to press the molten aluminum alloy. In this pressed state, the molten aluminum alloy solidified. As a result, the casting defects resulting from the shrinkage cavities or the like could be inhibited from occurring.
  • the liner 5 When the molten aluminum alloy started solidifying, the liner 5 was subjected to the shrinkage force arisen in the cast product. At this moment, however, the core 6 was still in the expanding state, and it still contacted with the inner peripheral surface of the liner 5. Consequently, the liner 5 was hardly deformed, and thereby it could be integrated with the cast product. When the casting mold was cooled, the core 6 shrunk greatly to produce a clearance between itself and the liner 5. Thus, the core 6 could be removed from the liner 5 with ease.
  • the liner 5 could maintain the predetermined configuration, and it did not require the finish machining. Thus, it was possible to give the liner 5 an as-designed thickness. Accordingly, the liner 5 could exhibit its maximum mechanical strength.
  • the casting mold of the Second Preferred Embodiment it is preferable to preliminarily heat the liner 5 and the core 6 to about 200 °C before charging the molten aluminum alloy into the casting mold. If the preliminary heating is done, the clearance between the liner 5 and the core 6 has disappeared before starting the charging of the molten aluminum alloy thereinto. Hence, it is possible to further reliably inhibit the invasion of the molten aluminum alloy into the clearance as well as the deformation of the liner 5 due to the pressure associated with the charging.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Molds, Cores, And Manufacturing Methods Thereof (AREA)
  • Moulds For Moulding Plastics Or The Like (AREA)

Description

The present invention relates to a method used to produce a cast product having a concave portion, e.g., a hole or the like, therein.
Description of the Related Art
For instance, as set forth in Japanese Unexamined Utility Model Publication (KOKAI) No. 59-25,361, a core or a core pin has been used conventionally when producing a cast product which has a concave portion such as a hole or the like therein. The core or the core pin is subjected to a holding force which results from the shrinkage of a molten metal during solidification. Accordingly, it is difficult to remove the core or the core pin from the resulting cast product after cooling the cast product. Hence, in order to make the core or the core pin likely to be removed from the cast product, it is usually tapered gradually from wide to narrow in the direction toward its leading end.
When the cast products are produced by using the core or the core pin, they come to have a concave portion such as a hole or the like. However, the resulting concave portion is inevitably formed in a tapered hole whose inside diameter reduces from large to small in the direction toward its inner side. Thus, it is hard to make the resulting concave portion which has an identical inside diameter over its entire length. As a result, it is a routine practice to carry out machining on the inner periphery of the concave portion after the casting, thereby establishing an identical inside diameter over the entire length of the concave portion.
In particular, when die-casting aluminum or zinc, the molten aluminum or zinc is solidified rapidly at its surface where it is brought into contact with a mold. Consequently, at the surface where the molten aluminum or zinc is brought into contact with the mold, there is formed a healthy layer in which no bubbles are involved in a thickness of from about 0.7 to 1.0 mm. However, there exist blow holes in the deeper layer disposed under the healthy layer, because the molten aluminum or zinc is solidified at a slower rate in the deeper layer.
Thus, when the taper-holed concave portion formed by casting is machined, and especially when the concave portion has a long overall length, the machining allowance should be enlarged on the inner side of the concave portion so that it goes beyond the healthy layer. As a result, the blow holes come to be exposed to produce defects. For example, when a cast product is produced by using a core or a core pin having a draft angle of 1 degree and when the resulting concave portion has an overall length of 200 mm, the concave portion should be machined in excess of about 3.49 mm at its innermost portion. Accordingly, the concave portion is machined completely beyond the healthy layer. However, in view of the removability of the core or the core pin from the cast product, it is actually impossible to get rid of the draft taper, and accordingly it is inevitable to carry out the machining after the casting. Hence, there always exists the fear for machining the cast product beyond the healthy layer.
A casting process using a cast insert member has been known, in which casting is carried out after a cast insert member e.g., a liner or the like, formed independently is disposed in a cavity. In this process, there exists a fear for deforming a cast insert member, because a cylindrical liner, for instance, is deformed by the shrinkage force of a molten metal during solidification. Accordingly, casting is carried out after disposing a protective member in a cast insert member. If such is the case, there should be provided a clearance between the cast insert member and the protective member. Consequently, it is difficult to completely get rid of the deformation in the cast insert member. Further, in order to prevent the protective member from being stuck in the cast insert member due to the deformation in the cast insert member, the protective member should be formed in a configuration having a draft taper. Consequently, when the cast insert member is deformed to conform to the configuration of the protective member, it is required to machine the inner periphery of the cast insert member after casting, and at the same time, there occur problems in that the machining has resulted in the partially fluctuating thickness in the cast insert member. Furthermore, there are produced defects which result from the molten metal invasion into the clearance between the cast insert member and the protective member.
DE-C-973984 discloses a casting core made of light metal and having a coefficient of expansion which is larger than the amount of shrinkage of a molten material. While cooling, the solidifying alloy shrinks less than the core. Thus, the core can easily be detached from the cast product. As the core is of light metal, it can be provided with an oxide film on its outer periphery or cooled by means of a liquid which is leaded through a bore within the core.
The oxide film or the liquid cooling are only used to prohibit the core from melting. Therefore, the cooling of the core is used to hold the temperature of the core some less the melting point of the core-material. Thus, the temperature of the core while solidifying of the cast product is nearly the same as the temperature of the cast product.
From JP -A- 63144845 a similar casting method is known. This method also uses a core having a thermal expansion coefficient which is greater than that of the casting material. In order to make sure that the core can be easily removed from the mold at an ordinary temperature, the core is preheated to a prescribed temperature which is adapted -on the one hand- to the average temperatures of the components when solidification starts, and -on the other hand- to the difference in the thermal expansion coefficients.
SUMMARY OF THE INVENTION
The present invention is developed in view of the aforementioned circumstances. It is therefore an object of the present invention to provide a method for producing a cast product with a concave portion which still allows to give the concave portion an inside diameter as identical as possible over its entire length and to reduce a machining allowance after casting, and which leads reliably to a large enough clearance between the core and the cast product, even with a broad range of cast materials.
This object will be achieved by the method according to claim 1.
A preferred form of the present casting mold can also solve the above-described problems, and at the same time it can inhibit the defects associated with the deformation of the conventional cast insert members from arising. In the preferred form thereof, the core further includes a casting insert member disposed around its outer periphery.
In the present casting mold, the core greatly expands thermally during casting. While it keeps the expanded state, the molten metal starts solidifying. Accordingly, the molten metal is subjected to a pressing force resulting from the expansion of the core during its solidification process. With the present casting mold, it is possible to inhibit the defects like the shrinkage cavities and so on from producing in the resulting cast products.
Further, when cooling the resulting cast products, the core shrinks more than the molten metal adjacent thereto does. Consequently, there arises a clearance between the outer peripheral surface of the core and the inner peripheral surface of the concave portion formed by the core in the resulting casting products. As a result, even when the untapered configuration is given to the core, it is possible to remove the core from the concave portion with ease and to reduce the machining allowance in the concave portion which has been usually required after casting.
Furthermore, when the core includes the cast insert member disposed on its outer periphery as done in the preferred form of the present casting mold, casting is carried out while the core is fitted into the cast insert member. Accordingly, the core expands greatly, thereby outwardly pressing the inner peripheral surface of the cast insert member. As a result, it is possible to reduce the clearance between the cast insert member and the core to zero. Hence, it is possible to inhibit the cast insert member from being deformed by the shrinkage stress of the molten metal and to prohibit the molten metal from invading between the cast insert member and the core.
Moreover, when cooling the resulting cast products, the core shrinks considerably to thereby produce a clearance between itself and the cast insert member. Consequently, it is possible to remove the core from the cast insert member with ease. Therefore, it is unnecessary to give the conventional tapered configuration to the core. Thus, it is possible to get rid of the step of machining the cast insert member after casting.
As having been described so far, in accordance with the present casting mold, it is possible to sharply reduce the manhour requirements required for the machining step after the casting step. Further, it is possible to inhibit the blow holes from exposing and to prohibit the casting material from being wasted, and thereby it is possible to reduce the production cost.
In particular, even when the cast insert member is employed, the cast insert member is inhibited from being deformed by the shrinkage force of the molten metal. Accordingly, it is possible to get rid of the step of machining the cast insert member after the casting and to prevent the strength of the cast insert member from being deteriorated.
BRIEF DESCRIPTION OF THE DRAWINGS
A more complete appreciation of the present invention and many of its advantages will be readily obtained as the same becomes better understood by reference to the following detailed description when considered in connection with the accompanying drawings and detailed specification, all of which forms a part of the disclosure:
  • Figure 1 is a schematic cross-sectional view of a casting mold of a First Preferred Embodiment according to the present invention;
  • Figure 2 is a graph illustrating the relationship between the temperature and the time during casting in which the casting mold of the First Preferred Embodiment is employed.
  • Figure 3 is a schematic cross-sectional view of a casting mold of a Second Preferred Embodiment according to the present invention; and
  • Figure 4 is a schematic cross-sectional view of a conventional casting mold.
  • DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS
    Having generally described the present invention, a further understanding can be obtained by reference to the specific preferred embodiments which are provided herein for purposes of illustration only and are not intended to limit the scope of the appended claims.
    First Preferred Embodiment
    In Figure 1, there is illustrated a schematic cross-sectional view of a casting mold of a First Preferred Embodiment according to the present invention. The casting mold comprises a pair of main molds 1, 2, a cavity 10 formed by the main molds 1, 2, and a cylindrical slider pin 3 disposed in the cavity 10. The casting mold is used for casting an aluminum die-cast component part. The slider pin 3 is formed of a high-manganese-content alloy which includes Mn in an amount of 22% by weight.
    Casting was carried out by charging a molten aluminum alloy into the casting mold constructed as described above. In Figure 2, there are illustrated a variation of the temperature of the molten aluminum alloy (or a cast product) with the time elapsed and a variation of the temperature of the slider pin 3 therewith. During the casting, the temperature of the molten aluminum alloy decreased gradually, but the temperature of the slider pin 3 increased sharply so as to approach the temperature of the molten aluminum alloy. Since the slider pin 3 exhibited a thermal expansion coefficient greater than that of the molten aluminum alloy, the slider pin 3 expanded to apply a pressing force to the molten aluminum alloy.
    Immediately after or before the solidification of the molten aluminum alloy was completed, water was supplied to a cooling water circuit (not shown) provided in the casting mold in order to cool itself and the cast product. Thus, the slider pin 3 was cooled rapidly. However, there exhibited a thermal resistance at the interface between the slider pin 3 and the cast product, and accordingly there was produced a large temperature difference between the slider pin 3 and the cast product. As a result, the slider pin 3 shrunk greatly, and it produced a large clearance between itself and the cast product. Hence, the slider pin 3 could be removed from the cast product with ease.
    In Figure 4, there is illustrated a casting mold which has been used conventionally. In the conventional casting mold, a slider pin 3' was employed which had a maximum diameter of 30 mm. Since it was formed of a steel, it exhibited a thermal expansion coefficient smaller than that of the molten aluminum alloy. When the solidification of the molten aluminum alloy was completed and when the conventional casting mold was about to be split, the cast product shrunk more than the slider pin 3' did, thereby fastening the slider pin 3'. Hence, the slider pin 3' was provided with a draft angle of 1 degree in order to make it likely to be removed from the cast product. Consequently, after the casting, the hole portion thus formed should be machined on the inner periphery by 2.24 mm at maximum, thereby producing the defects resulting from the shrinkage cavities. In addition, there arose the material loss which resulted in the problem in conjunction with the manufacturing cost.
    On the other hand, in the casting mold of the First Preferred Embodiment, the slider pin 3 could be removed from the cast product with ease even when it had a maximum diameter of 30 mm and it was provided with a draft angle of 15 minutes. If such was the case, it was necessary to machine the inner periphery of the hole portion only by a machining allowance of 0.8 mm at maximum after the casting. Therefore, it was possible to inhibit the material from being wasted, and at the same time there was produced no defect resulting from the shrinkage cavities.
    For instance, the slider pin 3 for casting an aluminum die-cast component part can be made from either a high-manganese-content alloy which includes Mn in an amount of from 10 to 25% by weight, C in an amount of from 0.2 to 1.5% by weight, Cr in an amount of from 1 to 3% by weight, and the balance of Fe and inevitable impurities, an austenite stainless steel, or a bimetallic alloy which includes Mn in an amount of from 65 to 80% by weight, Cr in an amount of from 10 to 20% by weight, and the balance of Ni and inevitable impurities.
    Second Preferred Embodiment
    In Figure 3, there is illustrated a schematic cross-sectional view of a casting mold of a Second Preferred Embodiment according to the present invention. The casting mold is designed to cast an automotive engine block, one of the aluminum die-cast component parts. It comprises an upper mold 40, a lower mold 41, and a pair of slider cores 42, 42. Between the upper mold 40 and the lower mold 41, there is disposed a liner 5 (i.e., the cast insert member) for constituting an inner peripheral surface of a bore. Moreover, a core 6 is held by the upper mold 40 at one of the opposite ends, and it is fitted into the liner 5.
    The liner 5 is made from a steel. The core 6 is formed of a bimetallic alloy which includes Mn in an amount of 68% by weight, and accordingly it exhibits a thermal expansion coefficient remarkably larger than those of the liner 5 and the resulting cast product. Moreover, when cooled, the core 6 is designed so that it has an outside diameter slightly smaller than the inside diameter of the liner 5.
    When the casting mold of the Second Preferred Embodiment was cooled, and when the core 6 was fitted into the liner 5, there was produced a clearance between the liner 5 and the core 6 so that the core 6 could be easily fitted into the liner 5.
    Then, when charging a molten aluminum alloy into the casting mold of the Second Preferred Embodiment, the liner 5 and the core 6 were expanded by the heat of the molten aluminum alloy. Since the core 6 exhibited a thermal expansion coefficient remarkably larger than that of the liner 5, it contacted with the inner periphery of the liner 5 to press the liner 5 in the expanding direction. Thus, the clearance disappeared, and accordingly the molten aluminum alloy barely invaded between the liner 5 and the core 6. Moreover, the expanding stress arisen in the liner 5 was conveyed to press the molten aluminum alloy. In this pressed state, the molten aluminum alloy solidified. As a result, the casting defects resulting from the shrinkage cavities or the like could be inhibited from occurring.
    When the molten aluminum alloy started solidifying, the liner 5 was subjected to the shrinkage force arisen in the cast product. At this moment, however, the core 6 was still in the expanding state, and it still contacted with the inner peripheral surface of the liner 5. Consequently, the liner 5 was hardly deformed, and thereby it could be integrated with the cast product. When the casting mold was cooled, the core 6 shrunk greatly to produce a clearance between itself and the liner 5. Thus, the core 6 could be removed from the liner 5 with ease.
    All in all, in the resulting cast product, the liner 5 could maintain the predetermined configuration, and it did not require the finish machining. Thus, it was possible to give the liner 5 an as-designed thickness. Accordingly, the liner 5 could exhibit its maximum mechanical strength.
    In addition, in the casting mold of the Second Preferred Embodiment, it is preferable to preliminarily heat the liner 5 and the core 6 to about 200 °C before charging the molten aluminum alloy into the casting mold. If the preliminary heating is done, the clearance between the liner 5 and the core 6 has disappeared before starting the charging of the molten aluminum alloy thereinto. Hence, it is possible to further reliably inhibit the invasion of the molten aluminum alloy into the clearance as well as the deformation of the liner 5 due to the pressure associated with the charging.
    Having now fully described the present invention, it will be apparent to one of ordinary skill in the art that many changes and modifications can be made thereto without departing from the scope of the present invention as set forth herein including the appended claims.

    Claims (10)

    1. A method for producing a cast product with a concave portion, comprising the steps of:
      inserting a core (3; 6) projecting into a cavity (10) of a casting mold,
      charging a molten metal into the cavity (10), and solidifying the molten metal,
      the core (3; 6) exhibiting a thermal expansion coefficient being equivalent to or more than a thermal expansion coefficient exhibited by the molten metal,
      wherein
      a) the core temperature is sharply raised during casting and the core is thus expanded to apply a pressing force on the molten metal, and
      b) immediately after or before the solidification of the molten metal has been completed, the core (3; 6) is cooled by supplying water to a cooling water circuit provided in the casting mold in order to cool the core (3; 6) rapidly and forcibly before splitting the mold, while
      c) increasing the temperature difference between the core (3) and the cast product.
    2. Method according to claim 1, characterized in that said molten metal includes aluminium or an aluminium alloy.
    3. Method according to claim 1, characterized in that said molten metal includes zinc or a zinc alloy.
    4. Method according to one of the claims 1 to 3, characterized in that a cast insert member (5) is disposed around the outer periphery of said core (3; 6) and in that the core (3; 6) exhibits a thermal expansion coefficient being larger than the thermal expansion coefficient exhibited by the cast insert member (5).
    5. Method according to one of the claims 1 to 4, characterized in that said core (3; 6) is formed of a high-manganese-content alloy.
    6. Method according to claim 5, characterized in that said high-manganese-content alloy includes Mn in an amount of from 10 to 25 % by weight, C in an amount of from 0.2 to 1.5 & by weight, Cr in an amount of from 1 to 3 % by weight, and the balance of Fe and inevitable impurities.
    7. Method according to one of the claims 1 to 4, characterized in that said core (3; 6) is formed of an austenite stainless steel.
    8. Method according to one of the claims 1 to 4, characterized in that said core (3; 6) is formed of a bimetallic alloy.
    9. Method according to claim 8, characterized in that said bimetallic alloy includes Mn in an amount of from 65 to 80 % by weight, Cr in an amount of from 10 to 20 % by weight, and the balance of Ni and inevitable impurities.
    10. Method according to one of the claims 1 to 9, characterized in that said core (3; 6) is untapered where it is brought into contact with the molten metal.
    EP94113405A 1993-08-27 1994-08-26 Casting mold Expired - Lifetime EP0642855B1 (en)

    Applications Claiming Priority (2)

    Application Number Priority Date Filing Date Title
    JP213128/93 1993-08-27
    JP5213128A JPH0760399A (en) 1993-08-27 1993-08-27 Metal mold structure for casting

    Publications (2)

    Publication Number Publication Date
    EP0642855A1 EP0642855A1 (en) 1995-03-15
    EP0642855B1 true EP0642855B1 (en) 1999-03-31

    Family

    ID=16634046

    Family Applications (1)

    Application Number Title Priority Date Filing Date
    EP94113405A Expired - Lifetime EP0642855B1 (en) 1993-08-27 1994-08-26 Casting mold

    Country Status (4)

    Country Link
    US (1) US5615726A (en)
    EP (1) EP0642855B1 (en)
    JP (1) JPH0760399A (en)
    DE (1) DE69417494T2 (en)

    Families Citing this family (12)

    * Cited by examiner, † Cited by third party
    Publication number Priority date Publication date Assignee Title
    DE4414168A1 (en) * 1994-04-22 1995-10-26 Alcan Gmbh Process for connecting two workpieces and composite component produced according to the process
    JP2002283003A (en) * 2001-03-22 2002-10-02 Toyota Industries Corp Casting method and metallic mold apparatus for casting
    DE19904971A1 (en) * 1999-02-06 2000-08-31 Vaw Alucast Gmbh Method and device for manufacturing engine blocks
    DE102005004481B3 (en) * 2005-01-31 2006-06-14 Hydro Aluminium Deutschland Gmbh Cooling mold is dimensioned so that the heat expansion coefficient of the mold fits the heat expansion coefficient of the casting material to be cast made from nickel- and/or manganese-alloyed cast iron
    DE102005054616B3 (en) * 2005-11-16 2006-11-09 Hydro Aluminium Mandl&Berger Gmbh Durable mold for light metal castings, especially cylinder heads, has a mold body with hollow zones to mold insert bodies to take the molten metal with shoulder in a positive fit at shaped holders and spaces to allow expansion of cold molds
    JP5670034B2 (en) * 2009-04-27 2015-02-18 錦見鋳造株式会社 Method for manufacturing thin-walled spheroidal graphite cast iron products
    JP5741407B2 (en) * 2011-11-28 2015-07-01 トヨタ自動車株式会社 Casting method and casting mold
    JP6266326B2 (en) * 2013-12-06 2018-01-24 株式会社ケーヒン Casting die apparatus and casting method
    CN104084554A (en) * 2014-08-04 2014-10-08 东莞台一盈拓科技股份有限公司 Die-cast formation method of amorphous alloy product
    JP6747938B2 (en) * 2016-07-12 2020-08-26 リョービ株式会社 Tilting gravity casting machine and tilting gravity casting method
    CN113927022A (en) * 2021-10-15 2022-01-14 泰州市锦峰新材料科技有限公司 Automatic demoulding equipment for casting high-temperature alloy bar
    CN114029454A (en) * 2021-11-05 2022-02-11 西峡县众德汽车部件有限公司 Casting method for solving shrinkage porosity of casting

    Family Cites Families (12)

    * Cited by examiner, † Cited by third party
    Publication number Priority date Publication date Assignee Title
    US1396341A (en) * 1920-07-27 1921-11-08 Rautenbach Arthur Casting and mold therefor
    FR1076338A (en) * 1952-03-18 1954-10-26 Carron Parlanti Ltd Process for casting hollow objects in light metal or in light alloy, and device for implementing this process
    DE973984C (en) * 1952-05-16 1960-08-11 Gustav Lauterjung Metallic core for casting molds, molds or the like.
    FR2108852A7 (en) * 1970-10-13 1972-05-26 Leroy Somer Casting cylindrical workpieces - in a mould with a core having a slip surface
    JPS5925361A (en) * 1982-07-30 1984-02-09 Hiroyuki Nohira Separation of amino acid and mandelic acid form compounded substance of amino acid and mandelic acid
    GB2193914B (en) * 1986-08-19 1990-08-15 Metal Castings Casting
    JPH0750049Y2 (en) * 1986-11-25 1995-11-15 イズミ工業株式会社 Strut for thermal expansion suppression piston
    JPS63144845A (en) * 1986-12-09 1988-06-17 Mitsubishi Heavy Ind Ltd Production of hollow casting
    JPS63281760A (en) * 1987-05-13 1988-11-18 Honda Motor Co Ltd Production of cylinder head for internal combustion engine
    JP2802384B2 (en) * 1988-09-20 1998-09-24 マツダ株式会社 Core for casting
    ZA916407B (en) * 1990-08-14 1992-04-29 Reilly Royalties Ltd Improvements to castings
    US5251683A (en) * 1991-03-11 1993-10-12 General Motors Corporation Method of making a cylinder head or other article with cast in-situ ceramic tubes

    Also Published As

    Publication number Publication date
    DE69417494D1 (en) 1999-05-06
    DE69417494T2 (en) 1999-07-22
    JPH0760399A (en) 1995-03-07
    EP0642855A1 (en) 1995-03-15
    US5615726A (en) 1997-04-01

    Similar Documents

    Publication Publication Date Title
    EP0642855B1 (en) Casting mold
    US6145184A (en) Method of manufacturing hollow bicycle crank arm
    US5737838A (en) Method of making a piston unit for an internal combustion engine
    JP3233358B2 (en) How to insert a pipe
    WO2006044713A2 (en) Insert cladding technique for precision casting processes
    US5305818A (en) Process for producing a moulded part, made of aluminium or an aluminium alloy, equipped with integrated channels
    US4589930A (en) Casting metal mold and method of producing the same
    US5850868A (en) Casting method with improved resin core removal step
    US4830390A (en) Front fork for bicycle
    JPH0399767A (en) Method for manufacturing internal chilling piping in casting metallic mold
    US3258818A (en) Method of casting metals
    US3825055A (en) Method of removing core from diecasting
    JP3036302B2 (en) Casting pins for casting
    GB2183516A (en) Pressure diecasting cores
    EP0257425A2 (en) Casting
    JP3079753B2 (en) Method of manufacturing piston for internal combustion engine
    JPH07178495A (en) Die for forging
    JP2004017100A (en) Method for manufacturing vehicle wheel
    JPH02307658A (en) Manufacture of cylinder block
    US20050155738A1 (en) Device and method for cooling a shot plug
    JPH07251254A (en) Die for forming cylinder block
    JPH08206814A (en) Metallic mold casting method
    JPH048139B2 (en)
    JPH0647160B2 (en) Method for manufacturing aluminum die cast products
    JPH09253822A (en) Production method of light alloy die casting using core

    Legal Events

    Date Code Title Description
    PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

    Free format text: ORIGINAL CODE: 0009012

    17P Request for examination filed

    Effective date: 19940826

    AK Designated contracting states

    Kind code of ref document: A1

    Designated state(s): DE FR GB

    17Q First examination report despatched

    Effective date: 19950703

    GRAG Despatch of communication of intention to grant

    Free format text: ORIGINAL CODE: EPIDOS AGRA

    GRAG Despatch of communication of intention to grant

    Free format text: ORIGINAL CODE: EPIDOS AGRA

    GRAH Despatch of communication of intention to grant a patent

    Free format text: ORIGINAL CODE: EPIDOS IGRA

    GRAA (expected) grant

    Free format text: ORIGINAL CODE: 0009210

    AK Designated contracting states

    Kind code of ref document: B1

    Designated state(s): DE FR GB

    ET Fr: translation filed
    REF Corresponds to:

    Ref document number: 69417494

    Country of ref document: DE

    Date of ref document: 19990506

    PLBE No opposition filed within time limit

    Free format text: ORIGINAL CODE: 0009261

    STAA Information on the status of an ep patent application or granted ep patent

    Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

    26N No opposition filed
    PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

    Ref country code: FR

    Payment date: 20000811

    Year of fee payment: 7

    PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

    Ref country code: DE

    Payment date: 20000822

    Year of fee payment: 7

    PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

    Ref country code: GB

    Payment date: 20000823

    Year of fee payment: 7

    PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

    Ref country code: GB

    Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

    Effective date: 20010826

    GBPC Gb: european patent ceased through non-payment of renewal fee

    Effective date: 20010826

    PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

    Ref country code: FR

    Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

    Effective date: 20020430

    PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

    Ref country code: DE

    Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

    Effective date: 20020501

    REG Reference to a national code

    Ref country code: FR

    Ref legal event code: ST